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Volumn , Issue , 2004, Pages

Simplified hybrid laminar flow control

Author keywords

Boundary layer suction; Boundary layer transition; Hybrid laminar flow control; Suction system

Indexed keywords

BOUNDARY LAYER SUCTION; BOUNDARY LAYER TRANSITIONS; COMMERCIAL AIRCRAFT; FLIGHT TEST; HYBRID LAMINAR FLOW CONTROLS; SELF ADAPTING; SUCTION SYSTEM; THROTTLE ORIFICE;

EID: 84893482271     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (18)

References (8)
  • 1
    • 0141881178 scopus 로고    scopus 로고
    • A320 HLF fin flight tests completed
    • R. Henke. A320 HLF fin flight tests completed. Air & Space Europe, 1 (2), 76-79, 1999.
    • (1999) Air & Space Europe , vol.1 , Issue.2 , pp. 76-79
    • Henke, R.1
  • 2
    • 84893464415 scopus 로고    scopus 로고
    • Calculation of A320 cp distributions for use in the ALTTA project
    • August
    • D. Sawyers. Calculation of A320 Cp distributions for use in the ALTTA project. Airbus UK Report TNW/2009/2000/0248, August 2000.
    • (2000) Airbus UK Report TNW/2009/2000/0248
    • Sawyers, D.1
  • 3
    • 84893432498 scopus 로고    scopus 로고
    • Development and experimental validation of an mathematical model for the pressure loss occurring across a perforated suction panel for hybrid laminar flow applications
    • June
    • J. Preist. Development and experimental validation of an mathematical model for the pressure loss occurring across a perforated suction panel for hybrid laminar flow applications. HYLDA Technical Report 59, June 1999.
    • (1999) HYLDA Technical Report 59
    • Preist, J.1
  • 5
    • 84893479115 scopus 로고    scopus 로고
    • Linear stability theory applied to natural and hybrid laminar flow experiments
    • P. Thiede June 19-21, 2000, Potsdam, Germany. Notes on Numerical Fluid Mechanics Springer-Verlag, Berlin/Heidelberg
    • G. Schrauf, K. H., Horstmann. Linear stability theory applied to natural and hybrid laminar flow experiments. In: P. Thiede. Proceedings of the CEAS/DragNet European Drag Reduction Conference, June 19-21, 2000, Potsdam, Germany. Notes on Numerical Fluid Mechanics, Vol 76, Springer-Verlag, Berlin/Heidelberg, 2001, pp. 157-163.
    • (2001) Proceedings of the CEAS/DragNet European Drag Reduction Conference , vol.76 , pp. 157-163
    • Schrauf, G.1    Horstmann, K.H.2
  • 6
    • 33645625645 scopus 로고    scopus 로고
    • Industrial view on transition prediction
    • S. Wagner, M. Kloker, U. Rist (eds.) in Germany. Numerical Notes of Fluid Mechanics and Multidisciplinary Design (NNFM) Springer, Berlin/Heidelberg/New York
    • G. Schrauf. Industrial View on Transition Prediction. In: S. Wagner, M. Kloker, U. Rist (eds.). Recent Results in Laminar-Turbulent Transition. Selected numerical and experimental contributions from the DFG priority programme "Transition" in Germany. Numerical Notes of Fluid Mechanics and Multidisciplinary Design (NNFM), Volume 86, Springer, Berlin/Heidelberg/New York, 2003, pp. 111-122.
    • (2003) Recent Results in Laminar-Turbulent Transition. Selected Numerical and Experimental Contributions from the DFG Priority Programme " Transition" , vol.86 , pp. 111-122
    • Schrauf, G.1
  • 7
    • 2342632539 scopus 로고    scopus 로고
    • Large-scale laminar flow experiments evaluated with linear stability theory
    • G. Schrauf. Large-scale laminar flow experiments evaluated with linear stability theory. AIAA Journal of Aircraft, 41 (2), 2004, pp 224-230.
    • (2004) AIAA Journal of Aircraft , vol.41 , Issue.2 , pp. 224-230
    • Schrauf, G.1
  • 8
    • 84871630965 scopus 로고    scopus 로고
    • Construction of an HLF nose for a vertical fin
    • April
    • H. Lajain. Construction of an HLF Nose for a Vertical Fin. ALTTA Technical Report 81, April 2003.
    • (2003) ALTTA Technical Report 81
    • Lajain, H.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.